EP0731330B1 - Tambour d'un canon du type revolver comprenant un système de refroidissement - Google Patents

Tambour d'un canon du type revolver comprenant un système de refroidissement Download PDF

Info

Publication number
EP0731330B1
EP0731330B1 EP19950113838 EP95113838A EP0731330B1 EP 0731330 B1 EP0731330 B1 EP 0731330B1 EP 19950113838 EP19950113838 EP 19950113838 EP 95113838 A EP95113838 A EP 95113838A EP 0731330 B1 EP0731330 B1 EP 0731330B1
Authority
EP
European Patent Office
Prior art keywords
barrel
revolver
channels
cooling
cartridge storage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP19950113838
Other languages
German (de)
English (en)
Other versions
EP0731330A1 (fr
Inventor
Michael Gerber
Rainer Hungerbühler
Oskar Dr. Melliger
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Air Defence AG
Original Assignee
Oerlikon Contraves AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Oerlikon Contraves AG filed Critical Oerlikon Contraves AG
Publication of EP0731330A1 publication Critical patent/EP0731330A1/fr
Application granted granted Critical
Publication of EP0731330B1 publication Critical patent/EP0731330B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A13/00Cooling or heating systems; Blowing-through of gun barrels; Ventilating systems
    • F41A13/12Systems for cooling the outer surface of the barrel

Definitions

  • the invention relates to a cooling device for revolver drums from Revolver cannons, according to the preamble of claim 1.
  • the patent cited above proposes to provide cooling channels in the region of the end part of the weapon barrel axially adjacent to a drum in the drum, radially outward, between the individual cartridge chambers, which have a main channel for the coolant supply running in the drum axis are connected.
  • the cooling channels are connected to nozzles running parallel to the drum axis, which open into the end of the drum facing the weapon barrel and are arranged at the same distance from the longitudinal axis of the drum as the central longitudinal axes of the cartridge chamber.
  • Shut-off devices for the nozzles are provided in the cooling channels, which in the event of bombardment briefly release the nozzle in the area of the pipe opening.
  • the shut-off devices are, for example, slides which can be moved by means of control pieces sliding along a control cam when the drum rotates.
  • the coolant passes through the nozzles directly onto the inner wall of the weapon barrel in the rear part.
  • the nozzles are only open for the period when the nozzles slide past in the rear of the gun barrel and the coolant is only supplied when shooting.
  • the coolant in the above-described cooling device for one Gun barrel is passed through the drum, can only be a cooling in Area of the drum front wall can be reached, so that this device for the Eliminating the problems mentioned above is not suitable.
  • US-A-2,801,575 (see the preamble of claim 1) describes a revolver barrel of a firearm with a cooling device; In the circumferential direction, alternating cooling channels follow in parallel to the drum axis and are connected to one another at their ends and along their length at a multiplicity of locations, which extend over the length of the bullet guide of the cartridge chamber, so that each cartridge chamber lies between two cooling channels and experiences a cooling effect from both . Conversely, each cooling channel is arranged between two cartridge chambers and must therefore contribute to the cooling of two cartridge chambers, so that a sufficient cooling effect per cartridge chamber is not guaranteed, although the construction is relatively complex due to the large number of connecting channels.
  • each cartridge chamber is two Assigned cooling channels, but, in contrast to the device according to this patent specification, both cooling channels are only responsible for cooling a single cartridge chamber.
  • the first of two cooling channels assigned to a cartridge chamber In the area of one end of the revolver drum stands the first of two cooling channels assigned to a cartridge chamber first tangential connecting pipes and the radial input channels with the one in the Inflow channel provided in the drum axis in connection.
  • the second of each two cooling channels assigned to a cartridge chamber is also in the area of an end face of the revolver drum via second tangential connecting pipes and radial output channels running parallel to the input channels with an in connected to the drain axis provided drain channel.
  • the advantages achieved by the invention are, in particular, that the coolant is not passed through all the cooling channels of the revolver drum one after the other, but that each cartridge chamber is assigned its own cooling circuit, with the result that effective, rapidly dissipating cooling is achieved.
  • Another advantage can be seen in the fact that a substantial part of the heat is quickly dissipated in the most heated area, in which the projectile is guided in the cartridge chamber. As a result, the area of the revolver drum in which the sleeve is guided in the cartridge chamber can no longer heat up as much. With these measures, the impairment of the cannon functions and strength problems are avoided and the tension curve in the drum is improved. Further advantages can be seen in the low manufacturing and logistics costs as well as in the small change effort for existing cannons.
  • 1 to 4 , 1 denotes a revolver drum which is rotatably mounted on a drum axis 2 .
  • the revolver drum 1 has 4 cartridge chambers 3 , which are divided into a projectile guide 3.1 and a sleeve guide 3.2 .
  • Each cartridge chamber 3 are associated with two extending parallel to the drum axis 2 cooling channels 4, which extend over the whole length of the floor guides 3.1 of the cartridge chamber 3 and are arranged in the region between the respective Patroneniager 3 and the periphery of the revolving drum.
  • the cooling channels 4 are closed on one end face 5 of the revolver drum 1 by means of sealing plugs 6 .
  • the cooling channels 4 assigned to a specific cartridge chamber 3 are connected to one another via tangentially extending connecting channels 7 .
  • the openings of the connecting channels 7 open into recesses 8 of the revolver drum 1 and are closed with further sealing plugs 9 .
  • In the region of one end face 5 of the revolving drum 1 is respectively connected to deflecting parts 11 of the first of two a cartridge chamber 3 associated cooling channels 4 extending through first tangential connecting pipes 10th
  • the deflecting parts 11 are connected to an inlet channel 13 provided in the drum axis 2 via radial inlet channels 12 which are offset by an angle of 90 ° to one another and arranged between the cartridge bearings 3 .
  • the inflow channel 13 there are four radial bores 14 offset from one another by an angle of 90 ° in the drum axis 2 , the axes of which lie in the same plane perpendicular to the drum axis 2 as the axes of the input channels 12 .
  • the deflecting parts 11 of the second of two a cartridge chamber 3 associated cooling channels 4 extending via second tangential connecting pipes 15 °.
  • the deflecting parts 11 are connected to an outlet channel 17 provided in the drum axis 2 via outlet channels 16 which run radially and parallel to the inlet channels 12 .
  • the outflow channel 17 is separated from the inflow channel 13 by an intermediate piece 18 .
  • At the beginning of the discharge channel 17 there are four radial bores 19 offset from one another by an angle of 90 ° in the drum axis 2 , the axes of which lie in the same plane directed perpendicular to the drum axis 2 as the axes of the output channels 16 .
  • 20 denotes a sealing sleeve in which sealing rings 21 resting on the drum axis 2 are held so that a coolant located in the cooling channels cannot escape.
  • the cooling device described above works as follows: The coolant is supplied via the inflow channel 13 , the four bores 14 , the four input channels 12 and the four first connecting pipes 10 to all the first cooling channels 4 ( 4 ′, FIG. 3 ) of the cartridge chamber 3 and from all second cooling channels 4 ( 4 ", 3 ) the cartridge chamber 3 is simultaneously removed again via the four second connecting pipes 15 , the four outlet channels 16 , the four bores 19 and the discharge channel 17. In this way, each cartridge chamber 3 is cooled separately and simultaneously with the others, so that a rapid and effective cooling is achieved.
  • the cooling can be operated by means of an open or closed circuit, water being used as the coolant, for example, and a pump provided for the coolant circulation being able to be switched on or off depending on the drum temperature. It is also irrelevant whether the cooling channels 4 through which the coolant flows through the described input channels 12 to the output channels 16 or vice versa.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Supply, Installation And Extraction Of Printed Sheets Or Plates (AREA)

Claims (7)

  1. Tambour (1) d'un canon de type revolver comprenant une installation de refroidissement pour le tambour, selon lequel
    le tambour (1) comporte plusieurs logements à munitions (3) et il est monté à rotation sur un axe (2),
    un canal d'alimentation (13) est prévu dans l'axe (2) du tambour, ce canal communiquant au niveau d'une face frontale (5) du tambour (1) avec des canaux d'entrée (12) disposés radialement,
    à chaque logement à munitions (3) sont associés deux canaux de refroidissement (4) parallèles à l'axe (2) du tambour, ces canaux s'étendant sur toute la longueur du guide d'obus (3.1) du logement à munitions (3),et
    les canaux de refroidissement (4) associés à un logement à munitions (3) sont reliés par leur extrémité à l'intérieur du tambour (1) par des canaux de liaison (7),
    caractérisé en ce que
    dans la zone de la même face frontale (5) du tambour (1), chacun des premiers des deux canaux de refroidissement (4) associés à un logement à munitions (3) est relié par un premier tube de liaison (10), tangentiel et les canaux d'entrée (12), radiaux sont reliés au canal d'alimentation (13) et chacun des seconds canaux de refroidissement (4) associés à un logement de munitions (3) est relié par des seconds tubes de liaison (15), tangentiels et par des canaux de sortie (16), radiaux, parallèles aux canaux d'entrée (12), avec un canal d'évacuation (17) prévu dans l'axe (2) du tambour
  2. Tambour selon la revendication 1,
    caractérisé en ce que
    les canaux de refroidissement associés à un logement de munitions (3) sont prévus chaque fois dans la zone comprise entre le logement à munitions (3) et la périphérie du tambour (1).
  3. Tambour selon la revendication 1,
    caractérisé en ce qu'
    à l'extrémité du canal d'alimentation (13), il y a quatre perçages radiaux (14) décalés de 90° dans l'axe (2) du tambour, les axes des perçages étant contenus dans le même plan que les axes des canaux d'entrée (12), plan perpendiculaire à l'axe (2) du tambour et
    au début du canal d'évacuation (17), il y a quatre perçages radiaux (19) décalés d'un angle de 90° dans l'axe (2) du tambour, et les axes des perçages étant situés dans le même plan que les axes des canaux de sortie (16), ce plan étant perpendiculaire à l'axe (2) du tambour.
  4. Tambour selon la revendication 1 comportant quatre logements à munitions (3),
    caractérisé en ce que
    les canaux d'entrée et de sortie (12, 16) sont décalés d'un angle de 90° entre les logements à munitions (3).
  5. Tambour selon la revendication 4,
    caractérisé en ce que
    les premiers et seconds tubes de liaison tangentiels (10, 15) sont reliés par des pièces de renvoi (11) aux canaux d'entrée ou de sortie (12, 16).
  6. Tambour selon la revendication 1,
    caractérisé par
    un circuit de refroidissement ouvert ou fermé.
  7. Tambour selon la revendication 6,
    caractérisé par
    une pompe de circulation pour l'agent de refroidissement, cette pompe étant mise en marche ou arrêtée suivant la température du tambour.
EP19950113838 1995-03-07 1995-09-04 Tambour d'un canon du type revolver comprenant un système de refroidissement Expired - Lifetime EP0731330B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH648/95 1995-03-07
CH64895 1995-03-07

Publications (2)

Publication Number Publication Date
EP0731330A1 EP0731330A1 (fr) 1996-09-11
EP0731330B1 true EP0731330B1 (fr) 1998-05-27

Family

ID=4191911

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19950113838 Expired - Lifetime EP0731330B1 (fr) 1995-03-07 1995-09-04 Tambour d'un canon du type revolver comprenant un système de refroidissement

Country Status (2)

Country Link
EP (1) EP0731330B1 (fr)
DE (1) DE59502333D1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1956334A1 (fr) 2007-02-09 2008-08-13 Oerlikon Contraves Ag Chambre à cartouches

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2466339C1 (ru) * 2011-05-13 2012-11-10 Учреждение Российской академии наук Институт прикладной механики Уральского отделения РАН Устройство охлаждения артиллерийских и стрелковых стволов

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE289332C (fr) *
DE328504C (de) * 1917-10-25 1920-11-03 Gabriel Szakats Einrichtung zum Kuehlen von Maschinengewehren
US2859664A (en) * 1956-06-15 1958-11-11 William P Murphy Drum cooling device
US2801575A (en) * 1956-08-29 1957-08-06 Donald P Grover Drum cooling device
DE3145764C2 (de) 1981-11-19 1983-12-29 Diehl GmbH & Co, 8500 Nürnberg Kühleinrichtung für Waffenrohre von Feuerwaffen

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1956334A1 (fr) 2007-02-09 2008-08-13 Oerlikon Contraves Ag Chambre à cartouches
DE102007007148A1 (de) 2007-02-09 2008-08-14 Oerlikon Contraves Ag Patronenlager

Also Published As

Publication number Publication date
EP0731330A1 (fr) 1996-09-11
DE59502333D1 (de) 1998-07-02

Similar Documents

Publication Publication Date Title
EP2867607B1 (fr) Silencieux pour une arme portative
DE69604097T2 (de) Mündungsbremse für ein mittel- oder grosskalibriges Geschütz
EP3056852A1 (fr) Silencieux
DE102011116059A1 (de) Schalldämpfer für eine Handfeuerwaffe
WO2011091949A1 (fr) Projectile gyrostabilisé
DE4315829C2 (de) Manöverpatronengerät
DE3145764C2 (de) Kühleinrichtung für Waffenrohre von Feuerwaffen
EP0731330B1 (fr) Tambour d'un canon du type revolver comprenant un système de refroidissement
EP0973003B1 (fr) Procédé et dispositif pour le refroidissement des tubes de canon
EP0027863A2 (fr) Frein de recul hydraulique pour freiner le recul du canon dès que le projectile a quitté le canon
EP0621941B1 (fr) Arme a feu
WO2017009116A1 (fr) Arme pourvue d'un faisceau de tubes
DE102005044553B3 (de) Magazin für eine automatisch schießende Waffe
EP0428525B1 (fr) Arme a feu
DE202019106316U1 (de) Signaturdämpfer
DE10157563A1 (de) Vollkalibriges Geschoss
DE2603636C3 (de) Waffe für den Abschuß von Start-, Signal- und bzw. oder Gasmunition
DE3733216A1 (de) Waffenrohr zum verschiessen von manoeverpatronen
DE3902352A1 (de) Gasdrucksteuervorrichtung
EP1312886B1 (fr) Barillet de munitions pour arme à feu
DE3342615C2 (fr)
DE1910790B3 (de) Handfeuerwaffe und Munition hierfür
DE2366037C2 (de) Vorrichtung zum gasdichten Abschließen einer Trennfuge
EP0081601B1 (fr) Arme à feu individuelle à canon court
AT1743U1 (de) Handfeuerwaffe

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): CH DE FR GB LI

17P Request for examination filed

Effective date: 19960923

17Q First examination report despatched

Effective date: 19961106

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: OERLIKON CONTRAVES AG

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): CH DE FR GB LI

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19980520

ET Fr: translation filed
REF Corresponds to:

Ref document number: 59502333

Country of ref document: DE

Date of ref document: 19980702

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19990930

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19990930

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: FR

Ref legal event code: TP

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20060811

Year of fee payment: 12

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20070904

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20070904

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 59502333

Country of ref document: DE

Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 59502333

Country of ref document: DE

Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 59502333

Country of ref document: DE

Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE

Effective date: 20111130

Ref country code: DE

Ref legal event code: R082

Ref document number: 59502333

Country of ref document: DE

Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE

Effective date: 20120523

Ref country code: DE

Ref legal event code: R081

Ref document number: 59502333

Country of ref document: DE

Owner name: RHEINMETALL AIR DEFENCE AG, CH

Free format text: FORMER OWNER: OERLIKON CONTRAVES AG, ZUERICH, CH

Effective date: 20120523

REG Reference to a national code

Ref country code: DE

Ref legal event code: R084

Ref document number: 59502333

Country of ref document: DE

Effective date: 20120809

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20140922

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20140919

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 59502333

Country of ref document: DE